Morteza Tayefi


Ph.D. in Dynamical Systems and Control, College of Engineering, Peking University, Beijing, China, 2017.

M.Sc. in Flight Dynamics and Control, Faculty of Aerospace Engineering, K. N. Toosi University, Tehran, Iran, 2006.

B.Sc. in Solid Mechanics, Department of Mechanical Engineering, Yazd University, Yazd, Iran, 2003.

Contact

Research


Field of Research:

Dynamical Systems and Control - Flight Dynamics - Cooperative Control - Lagrangian and Energy Shaping Methods



Current and Recent Research Projects

Courses


Automatic Control of Dynamical Systems, Spring 2019, Spring 2020








Publications


Journal Papers:

M. Tayefi, Z. Geng, Self-balancing controlled Lagrangian and geometric control of unmanned mobile robots, Journal of Intelligent & Robotic Systems, 90, Springer, 2018.

M. Tayefi, Z. Geng, Logarithmic control, trajectory tracking, and formation for nonholonomic vehicles on Lie group SE(2), International Journal of Control, Taylor & Francis, 2017.

M. Tayefi, Z. Geng, X. Peng, Coordinated tracking for multiple nonholonomic vehicles on SE(2), Nonlinear Dynamics, 87, Springer, 2017.

A. Mohammadi, M. Tayefi, Moving mass control system in conjunction with BELBIC for rate regulation of suborbital reentry payloads, Journal of System and Control Engineering, 226(9), IMechE, 2012.

A. Mohammadi, M. Tayefi, H. Kashani, Rate regulation of a suborbital reentry payload by moving mass actuators, Journal of Aerospace Engineering, 227(1), IMechE, 2012.

M. Tayefi, J. Roshanian, and A. Ghaffari, On estimation of vehicle linear model parameters, Aircraft Engineering and Aerospace Technology, 81(5), Emerald, 2009.

A. Ghaffari, J. Roshanian and M. Tayefi, Time-varying transfer function extraction of an unstable launch vehicle via closed-loop identification, Aerospace Science and Technology, Elsevier, 2007.

Conference Papers:

M. Tayefi, Z. Geng, A constructive self-balancing controlled Lagrangian for wheeled inverted pendulum, Chinese Control and Decision Conference, Yinchuan, China, 2016.

X. Peng, Z. Geng, M. Tayefi, Containment control based formation tracking for multi-vehicles on Lie Group, Chinese Control Conference, Chengdu, China, 2016.

M. Tayefi, Z. Geng, J. Sun, Contributions to tracking control for mechanical systems on SE(2), Chinese Control Conference, Hangzhou, China, 2015.

A. Mohammadi, M. Tayefi, M. Ebrahimi, Robust sliding mode control of a moving-mass actuated suborbital reentry biological payload, 64th International Astronautical Congress, Beijing, China, 2013.

A. Mohammadi, M. Tayefi, M. Ebrahimi, Developing an emotional Intelligent controller for space launch vehicle application, 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France, 2012.

M. Tayefi, A. Mohammadi, M. Ebrahimi, Development of a space launch vehicle 6DoF multipurpose simulation software, 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France, 2012.

M. Tayefi, A. Mohammadi, Linear quadratic rate regulation of a moving-mass actuated suborbital reentry payload, International Conference on Mechanical Engineering and Advanced Technology, Isfahan, Iran, 2012.

M. Tayefi, E. Taheri, M. Ebrahimi, After-separation dynamics and stochastic simulation of spin-stabilized satellites, AEROTECH III, Malaysian Institute of Aviation Technology, 2009.

M. Tayefi, K. Raissi, M. Bahrami, Wind effect on dynamic behavior of a launch vehicle, AEROTECH III, Malaysian Institute of Aviation Technology, Malaysia, 2009.

M. Tayefi, M. Ebrahimi, Design and analysis of separation systems based on an optimization approach, 47th AIAA Aerospace Sciences Meeting, Florida, 2009.

M. Tayefi, J. Roshanian, M. Bahrami, Linear model extraction of a launch vehicle by system identification based on six degrees of freedom simulation, The IASTED Asian Conference on Modeling and Simulation, Beijing, 2007.

Journal and Conference Papers in Persian:

M. Jafari, M. Tayefi, J. Roshanian, Improving INS performance using vehicle motion dynamics, Journal of Space Science and Technology, 2014.

M. T. Abadi, M. Fathi, M. Tayefi, Dynamic modeling of aero-elasticity for an aerospace vehicle, Conference of Mechanics and Advanced Technologies, Isfahan, Iran, 2013.

M. Tayefi, A. Mohammadi, A. Shahrokhi, Mission programming of a reentry capsule using flight simulation,10th Conference of Iranian Aerospace Society, Tehran, Iran, 2011.

A. Mohammadi, M. Tayefi, Development of dynamic equations of a reentry capsule in aero-ballistic coordinates, 10th Conference of Iranian Aerospace Society, Tehran, Iran, 2011.

M. Jafari, M. Tayefi, J. Roshanian, Implementation of dynamic equation of space modules in navigation system, 10th Conference of Iranian Aerospace Society, Tehran, Iran, 2011.

E. Amani, M. Tayefi, Fuel slushing dynamics and its effects on flight trajectory, First Conference on Flight Simulation, Tehran, Iran, 2009.

E. Taheri, M. Tayefi, J. Roshanian, Aerodynamic modeling of aerospace vehicles in 6DoF simulation, First Conference on Flight Simulation, Tehran, Iran, 2009.

A. Mohammadi, M. Tayefi, J. Roshanian, Preset and IGM methods integration in launch vehicles guidance, 7th Conference of Iranian Aerospace Society, Tehran, Iran, 2009.

Z. Sadeghi, M. Tayefi, A. Ghanbarian, Comparing aerodynamic and dynamic behaviors of sounding rockets with the various nose configurations, 7th Conference of Iranian Aerospace Society, Tehran, Iran, 2008.

M. Tayefi, J. Roshanian, A. Ghaffari, Estimating of linear system parameters for an ALV with the aid of numerical solution of nonlinear equations of motion, 6th Conference of Iranian Aerospace Society, Tehran, Iran, 2007.

M. Tayefi, J. Jodai and J. Roshanian, Multidisciplinary design optimization of a space vehicle by combination of parametric and Nelder-Mead methods, 14th Annual Conference on Mechanical Engineering, Isfehan, Iran, 2006.

Get In Touch


Faculty of Aerospace Engineering, K. N. Toosi University of Technology, Tehran, Iran

Email: tayefi@kntu.ac.ir

Tel: +98-21-73064362

PO Box: 16765-3381

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